Jabiru 2200 engine

GPTKB entity

Statements (48)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 8
gptkbp:bfsParent gptkb:Jabiru_Aircraft
gptkbp:accessories optional accessories available
gptkbp:application Jabiru J160, Jabiru J170
gptkbp:certification not certified by FAA
gptkbp:color gptkb:item
gptkbp:compression_ratio 8.5:1
gptkbp:cooling_system air-cooled
direct air cooling
gptkbp:design lightweight design
gptkbp:displacement 2200 cc
gptkbp:emissions_standard dual exhaust
gptkbp:engine 2
high reliability
2000 hours
rubber isolated
good climb performance
simple design features
flat engine layout
widely used in ultralight aircraft.
gptkbp:engine_type horizontally opposed engine
gptkbp:first_introduced 1990s
gptkbp:fuel_capacity high fuel efficiency
5 liters
approximately 10 L/h
gptkbp:fuel_type carbureted
MOGAS
https://www.w3.org/2000/01/rdf-schema#label Jabiru 2200 engine
gptkbp:ignition_system dual ignition
Champion RH M38
gptkbp:is_tested_for extensively tested
gptkbp:launch_site electric starter
gptkbp:maintenance 100 hours
gptkbp:manufacturer gptkb:Jabiru_Aircraft
gptkbp:market popular in homebuilt aircraft market
gptkbp:noise_level quiet operation
low vibration
gptkbp:powers 80 hp
gptkbp:propulsion fixed-pitch or constant-speed
gptkbp:setting V-type engine
gptkbp:torque 120 Nm
gptkbp:tuning not adjustable
gptkbp:type four-stroke engine
gptkbp:used_in gptkb:aircraft
gptkbp:valve_configuration SOHC
gptkbp:warranty 2 years warranty
gptkbp:weight approximately 120 kg